The invention relates to a UTO duct vertical unmanned aerial vehicle, and relates to the technical field of unmanned aerial vehicles, and the UTO duct vertical unmanned aerial vehicle comprises a flight module with a vehicle body and an undercarriage connected to the vehicle body. The undercarriage is composed of a first connecting base, a supporting assembly, a bidirectional driving assembly and the like, the supporting assembly achieves multi-direction buffering through a main plate, supporting blocks distributed in a matrix mode and a first elastic piece, and the bidirectional driving assembly drives a screw to rotate through a double-head motor and is matched with an adapter to achieve back-and-forth sliding of the main plate in the second direction; and meanwhile, a first telescopic rod, a second telescopic rod, a second elastic piece and a lifting assembly are arranged to enhance the structural stability and adaptability. The technical effect of optimizing the takeoff and landing stability of the unmanned aerial vehicle is achieved.

    本申请涉及一种UTO涵道垂起无人机,涉及无人机技术领域,其包括具有机体的飞行模块及连接于机体的起落架。起落架由第一连接座、支撑组件、双向驱动组件等构成,支撑组件通过主板、矩阵分布的支撑块及第一弹性件实现多方向缓冲,双向驱动组件利用双头电机驱动螺杆转动,配合转接件实现主板沿第二方向的往返滑动,同时设置第一伸缩杆、第二伸缩杆、第二弹性件及提拉组件以增强结构稳定性和适应性。本申请达到了优化无人机起落稳定性的技术效果。


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    Titel :

    UTO duct vertical unmanned aerial vehicle


    Weitere Titelangaben:

    一种UTO涵道垂起无人机


    Beteiligte:
    WU YUNGANG (Autor:in) / SHAO GUOJUN (Autor:in) / HE MIN (Autor:in) / TONG KUNHONG (Autor:in) / BERGEN KOKEN (Autor:in) / CHEN FEI (Autor:in)

    Erscheinungsdatum :

    13.05.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge



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